期刊文献+

充气可展开结构技术在空间探索领域中的应用 被引量:14

Applications of Inflatable Structure Technology for Space Exploration
在线阅读 下载PDF
导出
摘要 充气结构展开机理简单,重量轻、造价低,折叠体积有限,是近年广泛运用于各种航天器的一种新型空间结构形式。本文综述了充气可展开技术在充气可展开天线、薄膜太阳动力帆、太阳能发电系统、轻质运载工具和太空基地等方面的应用和研究进展,同时指出现阶段固化材料制备和空间环境影响等是利用此项技术急需解决的瓶颈问题。 Inflatable structure technology is a new choice for space exploration, and has been used widely in many spaceflight missions in recent years. There are many advantages of inflatable structures, such as simple deployable mechanism, light weights, low costs and limited fold volumes. This new technology is used to construct deployable antennae, solar sails, solar power systems, delivery means and habitat structures. Applications and research advances of these kinds of structures are addressed in this paper. However there are many problems yet to be solved, such as the production of rigidizable materials and the influence of space environments.
机构地区 浙江大学
出处 《载人航天》 CSCD 2009年第4期40-48,共9页 Manned Spaceflight
关键词 展开天线 充气可展开结构 太阳能发电系统 太阳动力帆 deployable antenna inflatable structure solar power system solar sail
  • 相关文献

参考文献2

二级参考文献15

  • 1FANG Hou-fei, LOU Michael, HUANG John. Devel opment of a three-meter ka-band reflect array antenna [C]. AIAA paper 2002-1706, 43rd AIAA/ASME/ ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Denver, 2002.
  • 2FANG Hou-fei, LOU Michael, HUANG John. Development of a 7-meter inflatable reflectarray antenna[C]. AIAA paper 2004-1502, 45rd AIAA/ASME/ASCE/ AHS/ASC Structures Structural Dynamics and Materials Conference. Palm Spring, 2004.
  • 3FANG Hou-fei, HUANG John, UBALDO Quijiano. Design and technologies development for an eight-meter inflatable reflect array antenna[C]. AIAA paper 2006- 2230, 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Newport, 2006.
  • 4LIN John K H, CADOGAN David P, FERTIA V Alfonso, et al. An inflatable microstrip reflectarray concept for ka-band apptications[C]. AIAA paper 2000-183, 41st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Atlanta, 2000.
  • 5FANG Hou-fei, LOU Michael. Catenary systems for membrane struetures[C]. AIAA paper 2001-1342, 42nd AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Materials Conference. Seattle, 2001.
  • 6SAKAMOTO Hiraku, MIYAZAKI Yasuyuki, PARK K C. Evaluation of cable suspended membrane structures for wrinkle-free design[C]. AIAA paper 2003-1905, 44th AIAA/ASME/ASCE/AHS/ASC Structures Struc rural Dynamics and Materials Conference. Norfolk, 2003.
  • 7[3]CLIFF E W,RON C S.A hybrid inflatable dish antenna system for spacecraft[C]∥Proceedings of the 42th AIAA/ASME/ASCE/AHS/ASC SDM Conference.Seattle:AIAA,2001:1-9.
  • 8[4]JOHN K H L,DAVID P C.An inflatable microstrip reflect array concept for Ka-band applications[C]∥ Proceedings of the 41th AIAA/ASME/ASCE/AHS/ASC SDM Conference.Atlanta:AIAA,2000:1-13.
  • 9[5]DAVID L.Inflatable deployed membrane waveguide array antenna for space[C]∥ Proceedings of the 44th AIAA/ASME/ASCE/AHS/ASC SDM Conference.Norfolk:AIAA,2003:1-7.
  • 10[6]PAI P F,LEYLAND G Y,LEE S Y.Geometrically exact modeling and design of high precision membranes[C]∥ Proceedings of the 43th AIAA/ASME/ASCE/AHS/ASC SDM Conference.Dallas:AIAA,2002:1-9.

共引文献21

同被引文献138

引证文献14

二级引证文献36

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部